1500.0
60.0
100.0
700.0
0.669
50.0
1
20
20
1751
0.05
64
60
Engine power, function of airspeed and pressure
atmosphere/P-sl-psf
velocities/ve-kts
0 50 100 150 200 250
503 0.357 0.380 0.400 0.425 0.457 0.486
1048 0.586 0.589 0.600 0.621 0.650 0.686
1328 0.707 0.721 0.731 0.757 0.786 0.821
1496 0.779 0.786 0.808 0.821 0.857 0.900
1684 0.850 0.857 0.874 0.900 0.943 0.979
1896 0.914 0.929 0.946 0.971 1 1.057
2135 1 1.011 1.029 1.043 1.083 1.150
2213 1.029 1.043 1.057 1.079 1.114 1.171
Engine Power, function of RPM and N1
0 5 60 86 94 95 96 97 98 99 100 101
0 0 0.5 0.5 0.5 0.5 0.5 0.5 0.5 0.5 0.5 0.5 0.5
800 0 0.5 35 200 350 380 420 460 500 530 580 620
1200 0 0.5 30 230 400 430 470 505 550 590 640 680
1600 0 0.5 5 240 440 475 510 550 595 630 680 720
2000 0 0.1 0.1 225 450 495 525 565 610 650 700 745
2200 0 0.1 0.1 205 440 480 515 560 605 645 695 743
Inter-Turbine Temperature ITT [deg C] depending on N1 and engine run (0=off / 1=running)
0 1
0 0 0
15 100 100
60 180 520
96 270 680
100 280 730